Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
CA 02591131 2010-04-06
Device for clamping at least two components for connection by friction stir
welding between two
edges of the components
The invention relates to a device for clamping at least two components, in
particular component
for aircraft, for connecting the components by a welding seam formed by means
of friction stir
welding between two component edges, whereby the components each are
accommodated by
multiple support elements and beneath the welding seam, a welding substrate is
arranged.
Known devices for clamping components for friction stir welding comprise a
massive, generally
level substructure, on which the components to be welded are supported. The
components are
clamped mechanically during the welding process by massive clamps. The clamps
must be
designed to be quite stable based on the high mechanical forces occurring
during friction stir
welding. Such clamps can be realized by screwed clamping jaws or by
hydraulically actuatable
clamping jaws.
In both case, first, a high constructive expense is provided. In addition, the
mechanical clamps
limit the dimensions of the components to be machined, since the clamps must
be introduced
from the outside as close as possible to the seam forming region in order to
hold down most
effectively the components in this area on a welding substrate. Very large-
sized and complex
components, for example in the form of fuselage shells in aircraft
construction, therefore cannot
be connected by friction stir welding by means of the known devices for
clamping components.
In addition, the clamping of components to be connected by means of friction
stir welding is
very time-consuming.
CA 02591131 2007-06-19
2
Furthermore, the massive design of the known devices for clamping components
for
friction stir welding require a high heat dissipation from the seam forming
region, so that
the drive speeds must be reduced in many cases.
Finally, these known devices cannot be adapted in a simple manner to different
component geometries, in particular to different single or double curved
components. In
addition, a specialized device for clamping must be provided for each
component
geometry, whereby the storage expense and costs are greatly increased.
In addition, flat vacuum clamping tables are known, whereby the time
expenditure
during clamping of the components to be processed is reduced. These vacuum
clamping
tables are likewise very massively constructed, so that also, the problem of
increased
heat dissipation from the seam forming region is presented.
Furthermore, the flat vacuum clamping table cannot be adapted in a simple
manner to
different component geometries.
Based on the disadvantages shown above, the known embodiments of devices for
clamping components for friction stir welding are suited only limitedly to the
cost-
effective and efficient involvement in the current, highly flexible production
processes.
The object of the present invention is to substantially avoid the
disadvantages of the
known embodiments of devices for claming components for friction stir welding.
This object is solved by a device with the features of patent claim 1.
CA 02591131 2007-06-19
3
Because the welding substrate on both sides, respectively, has at least one
holding
device that can be impinged with negative pressure for clamping the
components, the
components to be connected by means of friction stir welding on the face can
be firmly
clamped in a simple manner by the application of negative pressure. In
addition, the
device of the present invention makes possible the variable clamping of
different single
or double curved components with one and the same device, whereby essentially
only
the holding devices and/or the welding substrate, respectively, must be
adapted to the
different component geometries.
A further advantageous embodiment of the device of the present invention
contemplates
that the holding devices are attached releasably to a substructure. In this
manner, for
example, a fast and easy exchange of existing holding device is provided for
different
component geometries and/or component dimensions. In addition, the
substructure
produces a stable, load-bearing connection to a base plate, on which the
entire device of
the present invention rests.
A further advantageous embodiment contemplates that a surface geometry of the
holding
devices is adapted to a surface geometry of the components and/or to the
dimensions of
the components.
This embodiment makes possible the secure clamping of components with
different
geometries and/or different dimensions. In particular, by means of the device
of the
present invention, single and/or double curved components can be securely
fixed for
friction stir welding, whereby only the holding devices and if necessary the
welding
substrate must be exchanged.
CA 02591131 2007-06-19
4
According to a further advantageous embodiment of the device, a width of the
holding
devices is adapted in particular to different material thicknesses of the
components.
This embodiment permits a flexible adaptability of the device of the present
invention to
a plurality of different components, in particular to components with
different material
thicknesses. In this regard, the width of the holding devices, for example, is
greater, the
higher the material thickness of the component to be welded is, in order to
achieve a
sufficient contact pressure during the friction stir welding process. Because
with
increasing material thicknesses, the forces occurring in the friction stir
welding process
increase. In addition, the holding devices if necessary each can be adapted
individually
to single and/or double curved components.
According to features of a further advantageous embodiment, the welding
substrate is
arranged essentially centrally beneath the welding seam in a seam forming
region and is
formed to be exchangeable.
In this manner, a simple exchange of the wear-vulnerable welding substrate is
possible.
In addition, a substantially symmetrical support of the component to be welded
is
provided, which amounts to an improved quality of the welding seam.
Furthermore, also
a fine adaptation to the geometric design of the components in the seam
forming region,
if necessary, is possible, for example by different welding substrates for
different
component geometries. The welding substrate preferably is formed with a
metallic
material in order to permit a sufficient durability or wear resistance in the
friction stir
welding area.
According to a further advantageous embodiment, the welding substrate and the
holding
devices form a support surface. In this manner, the components to be connected
by
CA 02591131 2007-06-19
means of friction stir welding can rest as flatly as possible on the device of
the present
invention, so that a high quality and dimensional accuracy of the welding seam
formed
by means of friction stir welding is provided. The welding substrate and the
holding
devices hereby form an imaginary, essentially through-going support surface.
5
According to a further embodiment of the device of the present invention, the
components can be pressed onto the welding substrate in the seam forming
region by
means of at least one pressing device, in particular, a pressure roller. In
this manner,
during the friction stir welding, an even more improved positioning of the
components
in the seam forming region is provided.
According to a further advantageous embodiment, the support elements are
moveably
formed for adapting to different surface geometries and/or dimensions of the
components.
In this manner, components with different geometries and/or dimensions can be
accommodated flexibly. A plurality of support elements preferably is arranged
on both
sides of the holding devices, so that also large-sized components can be
securely
accommodated. The support elements are therefore formed substantially
perpendicularly
moveable. In addition, the support elements can be positionable additionally
in the
plane.
According to a further embodiment of the invention, the support elements have
connection elements, in particular, suction cups, for fixing the components.
These
embodiment variants make possible a secure hold also in the case of large-
sized
components, such as for example fuselage shells. Instead of suction cups, also
other
connection elements, such as clamps or the like, for example, can be used.
CA 02591131 2010-04-06
-6-
According to a further advantageous embodiment, the holding devices and/or the
substructure
are formed with a heat-insulating material.
In this manner, it is ensured that the heat existing during the friction stir
welding process in the
seam forming region or in the welding seam flows only to a small portion of
the device, so that
the drive/operating speed of the friction stir welding tool can be increased.
According to a further preferred embodiment of the invention, in the area of
the holding devices
and/or the substructure, at least one positioning device is arranged for
introducing and/or
orienting the component on the welding substrate and/or the holding devices.
By means of this embodiment, an at least partially automatic positioning of
the components to be
welded on the device is possible. The positioning devices can for example be
formed as
articulated arm with suction cups on the ends. The articulated arm can be
actuatable with
actuators, for example, in particular with hydraulic pistons, electric drives,
or the like. In
addition, the articulated arms also can be equipped with sensors for detecting
the actual position
in space or the position of the components in space. The control of the
articulate arm takes place
for example with a suitable control and regulating device. By means of the
control and regulating
device the control of the friction stir welding tool as well as the holding
devices can take place at
the same time.
In one aspect, the present invention resides in device for clamping at least
two components for
connecting the components by a welding seam formed by means of friction stir
welding between
two component edges, whereby the components each are accommodated by multiple
support
elements and beneath the welding seam, a welding substrate is arranged,
wherein the welding
substrate has a first side and a second side, each of the first side and the
second side has at least
one holding device with a plurality of channels, which can be impinged with
negative pressure
for clamping the components.
CA 02591131 2010-04-06
-6A-
In another aspect, the present invention resides in a device for clamping at
least two components,
in order to join the components by means of a weld seam formed between two
component edges
via friction stir welding, the device comprising: several supporting elements;
a welding backup
plate; wherein the components each are accommodated by several supporting
elements, and the
welding backup plate is arranged under the weld seam, wherein both sides of
the welding backup
plate each have at least one mounting device with a plurality of channels,
which can be placed
under a vacuum for clamping the components.
In the drawing:
CA 02591131 2007-06-19
7
Fig. 1 shows a perspective representation of the device of the present
invention for
clamping components during friction stir welding of components along
component edges.
Fig. 1 shows a perspective view of one exemplary embodiment of the device of
the
present invention for clamping two components, which are to be connected by
friction
stir welding with one another.
The device according to the present invention includes among other elements a
base
plate 1, a substructure 2, a welding substrate 3 as well as the holding
devices 4, 5. On
both sides of the substructure, a plurality of support elements are arranged.
The support
elements preferably are arranged spaced uniformly from one another in the form
of a
matrix. In the illustration of Fig. 2, for improved graphical representation,
shows only
half of the support elements 6 through 16.
A first component 17 and a second component 18 rest on the holding devices 4,
5, as
well as the support elements 6 through 16. The components can be sheets or
also more
complex components, such as segments of fuselage shells or the like.
The components 17, 18 are connected in a seam forming area 19 along the
component
edges 20, 21 by the welding seam 22. The welding seam 22 is formed by friction
stir
welding by means of a suitable friction stir welding tool 23 in a known
manner, which is
arranged on a tool carrier 24. The tool carrier 24 is guided for example by
means of a not
specifically illustrated, computer controlled portal robotic in the direction
of the arrow
25 along the component edges 20, 21 for forming the welding seam 22.
CA 02591131 2007-06-19
8
Since with friction stir welding, substantial mechanical forces occur, the
components 17,
18 must be fixed or clamped by means of the device of the present invention.
The seam
forming region 19 lies non-fixed on the welding substrate 3. The holding
devices 4, 5,
have on the upper sides facing the components 17, 18 a plurality of not
specifically
shown channels, which can be impinged with negative pressure. The channels can
be
milled in the top sides of the holding devices 4, 5 in a checkered manner or
applied in
another manner and type. Alternatively, also a matrix of bores can be applied
in the top
sides of the holding devices 4, 5, in order to enable formation of a negative
pressure
between the components 17, 18 and the holding devices 4, 5. In the edge
regions of the
holding devices 4, 5, further sealing strips are arranged in order to maintain
the negative
pressure between the components 17, 18 as well as the holding devices 4, 5. As
a result
of the negative pressure existing between the components 17, 18 and the
holding devices
4, 5, the components 17, 18 are pressed onto the holding devices 4, 5, by the
ambient air
pressure with a high pressing force. Based on the generally large-sized
components 17,
18 relative high pressure forces can be produced so that the components 17, 18
also do
not shift with high drive/operating speeds of the friction stir welding tool
23.
The holding devices 4, 5, are connected releasably with the substructure 2,
for example,
by screw connections, clamp connections, locking mechanism or the like, in
order to
permit an easy exchangeability of the holding devices 4, 5 depending on the
geometry
and/or the dimensions of the components 17, 18 to be clamped. In addition,
also the
substructure 2 can be attached releasably to the base plate 1, in order to
achieve a higher
flexibility with regard to different components.
For supporting the action of the holding devices 4, 5, in particular with
large-sized
components 17, 18, the device further has support elements 6 through 16. The
support
elements 6 through 16 can be moved independently of one another, respectively,
in the
CA 02591131 2007-06-19
9
direction of the black double arrow, that is, in z-direction. In this manner,
it is possible
also to securely and firmly clamp components with different dimensions and/or
geometries with the device of the present invention. In addition, the support
elements 6
through 16 can be formed to be moveable also in the x and y directions.
The welding substrate 3 and the top sides of the holding devices 4, 5 form a
somewhat
through-going support or contact surface 26, on which the components 17, 18
rest on
both sides of the component edges 20, 21. These fictive contact surfaces 26
continue on
both sides in the form of the matrix-like arranged support elements 6 through
16. For
improving the supporting action of all of the supporting elements 6 through
16, these
have connection elements on the ends, for example in the form of suction cups
27
through 30. In this manner, all of the support elements 6 through 16 as well
as the
further, not shown support elements are equipped with suction cups, whereby
the suction
cups 27 through 30 are shown in Fig. 1 for the not-shown suction cups. In this
connection, it should be noted that the support elements for achieving a
sufficient
clamping effect of the device do not necessarily have to be equipped with
suction cups.
The pressing forces produced by negative pressure by the holding devices 4, 5
suffice
generally for a secure fixing during the friction stir welding process.
For further improvement of the clamping action of the holding devices, 4, 5,
the tool
carrier 24 can have a pressure roller 3 1. With the pressure roller 3 1, the
component
edges 30, 31 are pressed firmly once again onto the welding substructure 3,
directly
before the friction stir welding tool 23 welds the components 17, 1 in the
seam forming
region 19. Also, the pressure roller 31 is not necessarily required for
achieving a
sufficient pressure force in the area of the component edges 20, 21 in the
seam forming
region 19.
CA 02591131 2007-06-19
By the previously illustrated features for clamping the components 17, 18, a
sliding of
the components 17, 18 during the friction stir process is impossible, so that
the
components 17, 18 can be connected by friction stir welding with the highest
dimensional accuracy.
5
The higher the material thickness of the components 17, 18 is, the higher a
width 32, 33
of the holding devices 4, 5 must be selected, in order to achieve sufficiently
high
pressing forces by the production of the negative pressure.
10 If components 17, 18 with a design that deviates from the geometric design
shown in
Fig. 1 are to be clamped by means of the device according to the present
invention, then
it is necessary to exchange at least the holding devices 4, 5 and to
substitute
corresponding holding devices adapted to the geometrid design of the
components. By a
corresponding design of the top sides of the respective holding devices
provided as well
as their widths, it is possible to adapt the device of the present invention
with minimal
expense to a plurality of different components with different geometric
dimensions. In
particular, it also is possible to securely and firmly clamp complex, single
and/or double
curved components with the mere exchange of correspondingly formed holding
devices.
In addition, it can also be necessary to keep ready special substructures as
well as special
welding substrates for adapting to component geometries and/or size dimensions
of
certain components. In the outer region of the component, the fixing takes
place then by
means of so called "support element fields" formed from a plurality of support
elements
arranged in a matrix-like manner and adaptable to a plurality of different
component
geometries and/or dimensions.
CA 02591131 2007-06-19
11
According to the present invention, however, it is no longer necessary to
provide a
complete, individual clamping device for each component geometry occurring in
the
production process, whereby substantial cost and time savings are provided.
On both sides of the substructure 2, further positioning devices 34, 35 are
arranged, by
means of which a fine positioning of the placed components 17, 18 is possible
with
reference to the welding substrate 3. In this regard, in Fig. 1, only two
positioning
devices 34, 35 are shown. Further positioning devices are arranged for
achieving an
efficient positioning of the components 17, 18 along the x-direction to both
sides of the
substructure 2, preferably spaced uniformly to one another, respectively. The
positioning
devices 34, 35 have connection elements, respectively, for example, suction
cups 36, 37
for again releasable attachment to the components 17, 18. The suction cups 36,
37 are
again representative for the further, not specifically shown connection
elements on the
positioning devices.
The substructure 2, the base plate 1, as well as the holding devices 4, 5, are
formed with
a metallic material, for example with an aluminum alloy, with steel, or the
like.
Deviating from the described material selection, at least the holding devices
4, 5, also
can be formed with a material that only conducts minimal heat, for example
with a
suitable ceramic and/or plastic material. In this manner, the heat dissipation
from the
seam forming region 19 is reduced, so that with the friction stir welding tool
23, higher
operating speeds can be achieved with the same quality of the welding seam.
The components 17, 18 further have small run-out areas 38, 39 in the seam
forming
region 19, which are separated after completion of the friction stir welding
process. The
run-out areas are embodied in the form of small plate-like continuations, as
shown by
way of example in Fig. 1. In this manner, the welding seam 22 always runs
completely
CA 02591131 2007-06-19
12
to a front or rear component edge of the components 17, 18. If the friction
stir welding
process 23, in contrast, were guided up to the front or rear component edge,
then the
welding seam 22 would be formed incompletely in these edge areas.
CA 02591131 2007-06-19
13
Reference numeral list
1 base plate
2 substructure
3 welding substrate
4 holding device
5 holding device
6 support element
7 support element
8 support element
9 support element
10 support element
11 support element
12 support element
13 support element
14 support element
15 support element
16 support element
17 first component
18 second component
19 seam forming region
20 component edge
21 component edge
22 welding seam
23 friction stir welding tool
24 tool support
25 arrow
CA 02591131 2007-06-19
14
26 support surface
27 suction cup
28 suction cup
29 suction cup
30 suction cup
31 pressure roller
32 width
33 width
34 positioning device
35 positioning device
36 suction cup
37 suction cup
38 run-out area
39 run-out area
